ISSN 1517-7076 artigo e-12032, 2018
Corresponding Author : Federico Guillermo Bonifacich Received on: 01/08/2017 Accepted on: 13/12/2017
10.1590/S1517-707620180002.0368
Influence of defects on the irreversible
phase transition in the Fe-Pd doped
with Co and Mn
Federico Guillermo Bonifacich1, Osvaldo Agustín Lambri1, Damián Gargicevich1, Griselda Irene Zelada1, José Ignacio Pérez-Landazábal2,3, Vicente Recarte2,3, Vicente Sánchez-Alarcos2,3
1 CONICET-UNR-Laboratorio de Materiales, Escuela de Ingeniería Eléctrica, Centro de Tecnología e Investigación Eléctrica, Facultad de Ciencias Exactas, Ingeniería y Agrimensura, Avda. Pellegrini 250, CP: 2000, Rosario, Santa Fe, Argentina.
e-mail: bonifaci@fceia.unr.edu.ar; olambri@fceia.unr.edu.ar; gargi@fceia.unr.edu.ar; gizelada@fceia.unr.edu.ar 2 Departamento de Física, Universidad Pública de Navarra, Campus de Arrosadía 31006, Pamplona, Navarra, Spain. 3 Institute for Advanced Materials (INAMAT), Universidad Pública de Navarra,
Campus de Arrosadía 31006, Pamplona, Navarra, Spain.
e-mail: ipzlanda@unavarra.es; recarte@unavarra.es; vicente.sanchez@unavarra.es
ABSTRACT
The appearance of BCT martensite in Fe-Pd-based ferromagnetic shape memory alloys, which develops at lower temperatures than the thermoelastic martensitic transition, deteriorates the shape memory properties. In a previous work performed in Fe70Pd30, it was shown that a reduction in defects density reduces the non thermoelastic FCT-BCT transformation temperature. In the present work, the influence of quenched-in-defects upon the intensity and temperature of the thermoelastic martensitic (FCC-FCT) and the non thermoelastic (FCT-BCT) transitions in Fe-Pd doped with Co and Mn is studied. Differential scanning calorimetric and mechanical spectroscopy studies demonstrate that a reduction in the dislocation density the stability range of the FCC-FCT reversible transformation in Fe67Pd30Co3 and Fe66.8Pd30.7Mn2.5 ferromagnetic shape memory alloys.
Keywords: Fe-Pd-Co; Fe-Pd-Mn; ferromagnetic shape memory alloys; martensitic transformation;
dislocation dynamics.
1. INTRODUCTION
Ferromagnetic shape memory alloys (FSMA) have attracted much scientific and technological interest owing to a broad range of possible engineering applications. These functional materials have the unique properties they show as a result of the combination of a thermoelastic martensitic transformation (MT) and a magnetic transition. In fact, one of the most interesting properties is the high magnetoplasticity they show as a consequence of the magnetic field induced re-orientation of the magnetic martensitic variants. In addition, fundamental physics studies related to the coupling between structural, mechanical, magnetic and thermodynamic properties are field of intense work [1,2]. Concerning the Fe-Pd system, the face centered tetragonal (FCT) martensitic phase allows the magnetic shape memory effect by reorientation of martensite variants via twin boundary motion. The FCT martensite can be obtained when cooling face centered cubic (FCC) austentite through the MT in samples which were quenched in iced water after an annealing at 1173 K [3-5]. This structural transformation from FCC to FCT only takes place in a very narrow compositional range (29 < at% Pd < 32) and the transformation temperatures lie typically below room temperature (RT) [6,7]. At lower temperature an irreversible transformation (FCT-BCT) needs to be prevented in order to retain the shape memory properties [8-12]. These temperatures strongly depend on both the composition and the addition of a third element. In fact, in previous works, the partial substitution of Fe by Co and Mn on the structural and magnetic properties of Fe-Pd alloys has been investigated and MT temperatures dependence has been observed [13,14]. Moreover, it was a reported that with some specific concentration of Mn it is possible to prevent the FCT-BCT non-thermoelastic MT [14].
of these phase transformations and in their stabilities [15-17]. Indeed, in a recent work the influence of defects on the FCT-BCT transition temperature has been studied. The large misfit between the cell parameters of FCT and BCT martensites point out to a critical role of dislocations in the accommodation of these phases. In this sense, mechanical spectroscopy which is a powerful and sensitive technique to analyze the dynamics of structural defects like dislocations was used [18,19].
The aim of the present work is to study the role of quenched-in-defect on the FCC-FCT and FCT-BCT transformations temperatures in Fe-Pd ferromagnetic shape memory alloys doped with Co and Mn by means of mechanical spectroscopy and differential calorimetry studies.
2. MATERIALS AND METHODS
Polycrystalline ingots of nominal composition (at.%) Fe67Pd30Co3 and Fe66.8Pd30.7Mn2.5 were prepared from high purity elements by arc melting under protective Ar atmosphere (called hereafter FePdCo and FePdMn). Ingots were homogenized in vacuum at 1273 K during 24 hours, and subsequently they were subjected to a 30 minutes annealing treatment at 1173 K in a vertical furnace; followed by quenching into iced water under vacuum. The compositions of the alloys were analyzed by energy dispersive X-ray spectroscopy (EDS) in a Jeol JSM-5610LV scanning electron microscope (SEM).
Differential scanning calorimetry (DSC) measurements were carried out at a heating/cooling rate of 10K/min in a TA Q100 calorimeter under nitrogen protective atmosphere. Different thermal cycles, involving heating and cooling runs, with different both minimum and maximum temperatures, within the interval around 150 K and 723 K, were performed in order to induce or prevent the non-thermoelastic MT. For Fe67Pd30Co3 were performed eight thermal cycles and for Fe66.8Pd30.7Mn2.5 were performed nine thermal cycles.
During the mechanical spectroscopy (MS) studies the simultaneous measurement of damping, Q-1 (or
internal friction) and natural frequency (f, f2 being proportional to the shear elastic modulus) as a function of
temperature were performed [18,20].
MS measurements were performed in a mechanical spectrometer based on an inverted torsion pendulum, assembled in the laboratory, under Ar at atmospheric pressure. The schematic representation of the experimental device is presented in Figure 1 taken from Ref. [21]. The maximum strain on the sample surface was 5x10-5. The measurement frequency was around 1 Hz. The heating and cooling rates employed in the tests were 1K/minute. Damping was calculated from the slope of the natural logarithm of the decaying amplitudes versus period number through equation (1), such that [18]
10 ln
ln An A n
Q (1)where An is the area of the nth decaying oscillation, A0 is the initial area of the starting decaying oscillation and n is the period number. For all these measurements the same initial and final values of the decaying amplitudes were used to avoid distortions linked to the appearance of amplitude dependent damping effects [20]. In order to study the presence of non-linear effects in the microstructure, amplitude dependent damping (ADD), i.e. damping as a function of the maximum strain on the sample, ε0, was calculated from equation (2) [20,22]:
dn A d
Q 1 ln n
0 1
(2)
Polynomials were fitted to the curve of the decaying areas of the torsional vibrations as a function of the period number by means of Chi-square fitting. Polynomials of degree higher than 1 indicate that Q-1 is a
function of ε0, leading to the appearance of ADD effects, as it can be inferred easily. Subsequently the equation (2) was applied. This procedure allows to obtain damping as a function of the maximum strain (ε0) from free decaying oscillations [20,22]. The strength of the ADD, can be determined through the average slope of the Q-1(ε0) curve using the S coefficient in equation (3) [20,22]:
0 1
Q
S (3)
where ΔQ-1 is the damping change corresponding to the full amplitude changes Δε0 measured in the whole
Figure 1: Schematic representation of the experimental device used during mechanical spectroscopy measurement. S: sample. G: jaws B: excitation coils. E: masses for variable moment of inertia. Taken from Ref. [21].
3. RESULTS AND DISCUSSION
The thermoelastic martensitic transformation (MT) has been studied firstly by DSC measurement. Figure 2 shows the DSC thermograms for FePdCo (a) and FePdMn (b) alloys, in the as-quenched state, from a temperature higher than the non-thermoelastic MT up to different maximum temperatures. In fact, the minimum temperature during the DSC measurements was 220 K and 273 K in order to prevent the non-thermoelastic MT in for FePdCo and FePdMn alloys, respectively. The exothermic (endothermic) peak observed on cooling (heating) corresponds to a direct (reverse) thermoelastic MT. Thermoelastic MT occurs at 260 K and 310 K for FePdCo and FePdMn, respectively. The MT temperature was obtained as the reaction peak temperature, i.e. MT temperature peak. The measured enthalpies are 0.8 J/g and 0.7 J/g for FePdCo and FePdMn, respectively [14,23,24]. The Curie temperatures can be observed thorough the change in the baseline at TC=603 K for FePdCo and TC=540 K for FePdMn [13,24].
After several thermal cycles up to different maximum temperatures, appreciable changes in the height and temperature of the MT from DSC thermograms were not detected [25]. A change in less than 3 K for the MT temperature was detected in the two alloys.
On further cooling a non-thermoelastic (FCT-BCT) transformation takes place. In fact, thermograms shown in Figure 3 were performed at temperatures lower than the non-thermoelastic MT temperature. These thermograms show a series of peaks which correspond to the FCT-BCT transformation in FePdCo alloy. The approximate temperatures for the appearance of the non-thermoeleastic MT were 190 K and 240 K for FePdCo and FePdMn, respectively [13,14,25,26]. The FCT-BCT transformation is non-thermoelastic and the appearing BCT phase will remain (degrading the shape memory properties) unless the alloy is annealed at high temperature and subsequently quenched [6].
-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
200
300
400
500
600
700
HF (
W/g
)
Temperature (K)
0.07 0.072 0.074 0.076
230 240 250 260 270 280 290
HF
(
W
/g
)
Temperature (K)
Reverse MT
Tc
(a)
exo up
-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
300
400
500
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700
Temperature (K)
HF (
W/g
)
0.082 0.086 0.09 0.094 0.098
280 290 300 310 320 330 Temperature (K)
H
F
(W
/g
)
Tc
Reverse MT
(b)
exo up
Figure 2: Heat flux (HF) as a function of temperature during the DSC measurement for (a) FePdCo and (b) FePdMn
0
0.004
0.008
0.012
0.016
0.02
0.024
0.028
160
200
240
280
320
HF (
W/g
)
Temperature (K)
FCC-FCTFCT-BCT
exo up
FePdCoFCC-FCT FCT-BCT
FePdMn
Figure 3: DSC thermograms performed down to temperatures lower than the non-thermoelastic transformation
tempera-ture for FePdCo and FePdMn.
In order to study the influence of the non-thermoelastic MT on thermoelastic MT, mechanical spectroscopy measurement from temperatures below the FCT-BCT transformation temperature were carried out. Figures 4 and 5 show the damping spectra and squared frequency (proportional to shear elastic modulus) curves, from 170 K up to different maximum temperatures, for FePdCo and FePdMn alloys, respectively. The maximum temperature reached in each consecutive thermal cycle was increased as follows: 603K, 603K, 673K, 773K and 773K. In Figures 4(a) and 5(a) a damping peak at around 450 K can be observed during the successive thermal cycles. During the second heating run up to the same temperature of the first, this peak decreases its height markedly in both alloys. In fact, this peak has been reported as P1 peak in Fe70Pd30 with and without BCT phase, and in Fe67Pd30Co3 and Fe66.8Pd30.7Mn2.5 without the appearance of BCT phase [24
-26]. The mechanism of the P1 peak was related with a dislocation dragging mechanisms controlled by the migration of vacancies without break-away and is related to the intrinsic properties of the austenitic phase [25]. Therefore, the net peak height (after background subtraction) is lower in a matrix with BCT phase than in a matrix without BCT phase, since the BCT phase is still present overlapped to the austenite matrix. In fact, in FePdCo and FePdMn alloys a 32% and 38% (mass) transform to the BCT martensite during the cooling down to 170 K, respectively. These amounts remain unless the alloy is annealed at high temperature and subsequently quenched [13]. After the first heating run up to 603 K, the P1 peak decreases its height markedly in both alloys, indicating that the density of quenched-in-defects was decreased [24].
On the other hand, damping spectra show higher values of damping in martensitic phase than in austenitic phase. In fact, the damping behaviour out of the range of MT peak is controlled by the background damping values of each phase. This behaviour is in agreement with the damping capacity of the twin boundary and dislocations in the martensitic phase, while in the austenitic phase only dislocation contribute to background damping values. Nevertheless, the damping background values in the martensitic phase decrease, as different annealing were performed. This indicates that, effectively, the density of point defects and dislocations decreases and consequently the interaction between twin boundaries and structural defects decreases too. This effect is presented more clearly after the first heating run up to 603 K and 773 K, so the maximum temperature was reached in consecutive cycles two times. Then, damping capacity in the martensitic phase decreases and the contribution to the damping values is mainly controlled by twin boundaries motion [18,19].
was related with a mechanism that involves a precipitation and decomposition processes of the γ phase [27]. The effect of the thermal cycles on the non-thermoelastic MT can be seen from the movement of the hillside towards lower temperatures in Figures 4(a) and 5(a). In fact, the FCT-BCT transition temperature moves towards lower temperatures mainly after the first thermal cycle at 603 K. This behavior indicates that the reduction of structural defects difficult the appearance of BCT.
0
1
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3
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7
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800
603 K 603 K673 K 773 K
773 K
Dam
pin
g, Q
-1
x10
3
Temperature (K)
(a)
P1
MT
0.8
1
1.2
1.4
1.6
200
300
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500
600
700
800
603 K 603 K673 K 773 K
773 K
Temperature (K)
Squ
ared
freq
uen
cy (s
-2
)
(b)
MT
Figure 4: Damping spectra (a) and squared frequency curves (b) as a function of temperature during successive thermal
0
0.5
1
1.5
2
2.5
3
3.5
4
200
300
400
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800
603 K603 K
673 K 773 K
773 K
Temperature (K)
Damping, Q
-1
x10
3
(a)
P1
MT
0.5
0.6
0.7
0.8
0.9
1
1.1
200
300
400
500
600
700
800
603 K 603 K673 K 773 K
773 K
Square
d frequ
ency (s
-2
)
Temperature (K)
(b)
MT
Figure 5: Damping spectra (a) and squared frequency curves (b) as a function of temperature during successive thermal
cycles for a FePdMn alloy from 170 K up to different final temperatures. Lines are a guide for the eyes.
The appearance of ADD has been checked through the behaviour of S parameter for the first and second heating runs of the whole cycles shown in Figure 4 and 5. S values as a function of temperature for as-quenched samples and after annealing to 603 K is shown in Figure 6. As it can be expected, the values differ from zero for temperatures lower than MT temperature since the mobility of twin boundaries. The higher values of S for the annealed samples and the decrease of the amount of quenched-in-defects, i.e. decrease of P1 peak, indicate that both dislocations and variants increase their mobility. On the other hand, the S values are zero for temperatures higher than MT temperature. The absence of ADD effects indicate that the dislocation movement is carried out without thermally activated break-away [18-20,22,28].
0
10
20
30
40
50
60
70
80
150 200 250 300 350 400 450 500 550
S=
Q
-1
/
0Temperature (K)
MT
MT
FePdMn FePdCo
Figure 6: S parameter as a function of temperature for the as-quenched (circles) and annealed at 603 K (open circles)
state for a FePdCo and FePdMn alloys. Lines are a guide for the eyes.
Finally, in order to check that both the non-thermoelastic MT transition and the Mn and Co substitutional atoms have not influence on the relaxation mechanism controlling P1 peak, the activation energy and pre-exponential factor for the relaxation time corresponding to P1 peak were obtained from the Arrhenius plot (the peak temperature shifts measured at different oscillation frequencies) for both alloys [18]. In fact, Figure 7 shows the Arrhenius plot related to P1 peak for the two alloys. The values obtained were HaFePdCo= (1.0±0.1) eV and oFePdCo=810-(14±0.5) s, and HaFePdMn= (1.0±0.1) eV and oFePdMn=110-(13±0.5) s. These values are in agreement with those previous obtained in these alloys, FePdCo and FePdMn, without the appearance of the BCT phase [24]. Moreover, the activation parameters are also in agreement with previous reported works in Fe70Pd30 with and without the appearance of the BCT phase [24,25]. Consequently, the driving force controlling the development of P1 is effectively the same as said before [25].
-3.5
-3
-2.5
-2
-1.5
-1
2.1
2.15
2.2
2.25
2.3
2.35
ln(1/
P)
1/T
Px 10
3
(K
-1)
FePdCo - (1.0 ± 0.1) eV - 0 = 8x10-(14.0±0.5) s FePdMn - (1.0 ± 0.1) eV - 0 = 1x10-(13.0±0.5) s
Therefore, the behaviour of the P1 peak let to conclude that annealing of FePdCo and FePdMn alloys over 603 K leads to a recovery of the structure where the amount of point defects and dislocations decrease. So, it is expected that this recovery makes difficult the accommodation of the misfit strain between the FCT and the BCT phases, giving rise to a decrease in the temperature for the appearance of the irreversible BCT phase [25]. In fact, from Figures 4(a) and 5(a) it can be seen the movement of the hillside of the MT non-thermoelastic phase at lower temperatures, between 210 K and 250 K for FePdCo and between 200 K and 290 K for FePdMn. This movement of the hillside is directly related with the movement towards lower temperatures of the FCT-BCT transition. Indeed, Figure 8 shows a decrease in the temperature for the appearance of the BCT phase measured through DSC in Fe70Pd30 (full line) and MS in Fe70Pd30 (dashed line) [25], Fe67Pd30Co3 (dotted line) and Fe66.8Pd30.7Mn2.5 (alt-dashed line); from where a good correspondence between the curves can be observed.
170
180
190
200
210
220
230
240
250
0
1
2
3
4
Tem
pe
rau
re (K
)
Previous maximum temperature (K)
DSC FePd MS FePd
MS FePdMn
MS FePdCo
603
603
673
773
773
Figure 8: FCT-BCT transformation temperature as a function of the maximum temperature of the thermal cycles. See
explanation in the text.
4. CONCLUSIONS
The stability at low temperatures of the thermoelastic martensite in FePdCo and FePdMn alloys is restricted by the irreversible BCT phase transformation. The appearance of dislocations, as a result of the FCT-BCT strain misfit, and their dynamics has been analyzed by mechanical spectroscopy. The P1 damping peak, at around 450 K, related to the dislocation movement has been identified in these alloys with BCT non-thermoeleastic MT. The appearance of non-non-thermoeleastic MT and the addition of substitutional atoms do not modify the physical mechanisms controlling the P1 peak. Moreover, the behavior of the movement of the FCT-BCT transition temperature is not affected by the addition of substitutional atoms. Finally, a reduction of the dislocation density reduces the irreversible transformation temperature and so, increases the stability range of the FCC-FCT reversible transformation.
5. ACKNOWLEDGMENTS
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